School of Aerospace Engineering Measurable Quantities in TD • “Easiest” TD properties to measure: T, p, V, M • Are there others? – specific “heats” (also known as heat capacities) – “heats” of reaction and phase change – compressibility coefficients • Based on our ability to measure – how much heat transfer required for some change – change in volume/density under some fixed conditions AE/ME 6765 Measurable Quantities-1 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. School of Aerospace Engineering Specific Heats • Define (dni=0) dU = ∂U ∂U dT + dV ∂T V ∂V T specific heat at ≡ CV const. volume dH = ∂H ∂H dT + dp ∂T p ∂p T specific heat at ≡ C p const. pressure – extensive TD properties, also know as “frozen” specific heats if dni=0 • Interpretation – if only pdV work allowed (dU = δQ − pdV ) const. volume dU = CV dT δQ − pdV = CV dT CV = δQ dT Measurable Quantities-2 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. const. pressure dH = C p dT amount of energy addition as heat transfer required to change T of subst. by dT δQ + Vdp = C p dT C p = δQ dT AE/ME 6765 1 School of Aerospace Engineering Specific Heats • So historically these properties were determined from measuring temperature change for given heat addition (or equiv. work by Joule) at fixed V or p • From Maxwell Relations, already showed ∂S ∂S ∂U ∂S similar approach C p = T =T ⇒ CV = T ∂T V ∂T V ∂T V ∂T p • Intensive versions cp = Cp M cv = CV M ĉv = CV ∑n i ĉ p = C p ∑n i • Units: 1 BTU/lbmºF = 1 cal/gC = 4.187J/gK defined historically for H2O at room T Measurable Quantities-3 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. air ~1 J/gK@300K AE/ME 6765 School of Aerospace Engineering Compressibility Coefficients • Examine V=V(T,p), with (ni const.) ∂V ∂V dV = dT + dp ∂T p ∂p T 1 ∂V − 1 ∂V Isobaric Isothermal α≡ κ≡ Compressibility Compressibility V ∂T p V ∂p T • Also − 1 ∂V Isentropic Note: many texts reverse Compressibility β ≡ V ∂p defn. α↔β S – all intensive – for fixed composition, can write all partials in terms of: α, κ, cp, p, v, T – strength materials: coeff. linear expansion = α/3 Young’s modulus of elasticity ∝ κ – speed of sound → β Measurable Quantities-4 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. AE/ME 6765 2 School of Aerospace Engineering Compressibility Coeff: Perfect Gas • Starting with PG state eqn. ∂V ∂T nR T V= p ∂V ∂p • So α≡ 1 ∂V V ∂T κ≡ p − 1 ∂V V ∂p = V T = −V p p T T κ =1 p α =1 T AE/ME 6765 Measurable Quantities-5 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. School of Aerospace Engineering Compressibility Coefficients • For gen’l. simple compressible substance (dni=0) α≡ • and 1 ∂V V ∂T κ≡ p − 1 ∂V V ∂p T dV = αVdT − κVdp 1) From reciprocity ∂α ∂p = T − ∂κ ∂T p T2 p2 dV = ∫ αdT − ∫ κdp V1 V T1 p1 If α, κ constant 3) From cyclic rule ln(V2 V1 ) = αΔT12 − κΔp12 ∂p α ∂p ∂T ∂V = = −1 ∂T V ∂V p ∂p T ∂T V κ 2) Integrating Measurable Quantities-6 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. V2 ∫ AE/ME 6765 3 School of Aerospace Engineering Specific Heats and Compress. Coeffs. • Can develop relationship between these properties ∂S ∂p • Start with dS = ∂S dV + ∂S dT = ∂V dS = ∂T T V C ∂p dV + V dT ∂T V T Showed from ∂V Maxwell Relations ∂S ∂T ∂T T = V V 1 ∂U T ∂T V • With similar methods (dH) dS = • Equate dp = Cp − ∂V dp + dT ∂T p T C p − CV T (∂V ∂T ) p dT − (∂p (∂V ∂T )V dV ∂T ) p = (∂p ∂T )V AE/ME 6765 Measurable Quantities-7 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. School of Aerospace Engineering Specific Heats and Compress. Coeffs. • So ∂p ∂T • Showed = V C p − CV T (∂V ∂T ) p ∂p ∂T • So = V α κ α ∂V T κ ∂T α = Tα V κ α 2V C p − CV = T κ C p − CV = p Perf. Gas (1 T )2V = pV = nR C p − CV = T 1 p T 1) Turns out κ>0 for all stable substances ⇒Cp≥CV (or cp≥cv) 2) For α=0 ⇒ Cp=CV 3) As T→0 ⇒ Cp→CV (exper. show κ not →0) 4) Can also show C p CV = c p cv = κ β Measurable Quantities-8 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. AE/ME 6765 4 School of Aerospace Engineering Heats of Reaction and Phase Change • Can examine change at specified conditions, e.g., constant T and p – phase change – composition change (liq)→(sol) A+B→C • Energy change (increase or decrease) – for no work but pdV saw in 1st Law const. Q = ΔU12 volume 12 const. Q = ΔH 12 pressure 12 Measurable Quantities-9 Copyright © 2009 by Jerry M. Seitzman. All rights reserved. net heat transfer (heating) required in phase change/reaction related to energy difference between phases or RHS vs LHS AE/ME 6765 5